PROPOSED INVESTIGATION OF VISCOUS-INVISCID EFFECTS IN HYPERSONIC FLOW IN THE AEDC GAS DYNAMICS FACILITY TUNNEL B. PHASE II
GENERAL APPLIED SCIENCE LABS INC HEMPSTEAD N Y
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A test program is presented for a series of hypersonic research tests to provide detailed data for pressure distribution and heat transfer over several model configurations. The model configurations include delta planforms 70 degrees lambda 0 degrees dihedral, 70 degrees lambda 10 degrees cathedal, 70 degrees lambda 10 degrees dihedral, 60 degrees lambda 0 degrees dihedral, 75 degrees lambda 0 degrees dihedral, fin-flat plate interference 90 degrees Fin, and 45 degrees fin-flat plate interference.